ML20079D607

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Westinghouse Revised Thermal Design Procedure Instrument Uncertainty Methodology for Alpr,Farley Nuclear Plant,Units 1 & 2 (for RTD Bypass Loop Elimination)
ML20079D607
Person / Time
Site: Farley  Southern Nuclear icon.png
Issue date: 05/31/1991
From: Moomau W
WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP.
To:
Shared Package
ML19302E789 List:
References
WCAP-12772, NUDOCS 9107180296
Download: ML20079D607 (37)


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WESTINGHOUSE CLASS 3 WCAP-12772 o

WESTINGHOUSE REVISED THERMAL DESIGN PROCEDURE INSTRUMENT UNCERTAINTY METHODOLOGY FOR ALABAMA POWER FARLEY NUCLEAR PLANT UNITS 1 AND 2 (FOR RTD BYPASS LOOP ELIMINATION)

MAY, 1991 W.H.Moomau l

Westinghouse Electric Corporation Energy Systems P.O. Box 355 Pittsburgh, Pennsylvania 15230 (c)1991 Westinghouse Electric, All Rights Reserved

~

ACKNOWLEDGEMENTS The author wishes to recognize the contributions of Mr. Michael G. Eidson of Southern Nuclear Company for his careful review of this report.

i

TABLE OF CONTENTS SECTION TITLE PAGE I. Introduction 1 II. Methodology 2 III. Instrumentation Uncertainties S IV. Conclusions 27 References 28 ii

LIST OF TABLES TABLE NUMBER TITLE PAGE 1 Pressurizer Pressure Control 6 System Accuracy 2 Rod Control System Accuracy 8 3 Flow Calorimetric Instrumentation 17 Uncertainties 4 Flow Calorimetric Sensitivities 18 5 Calorimetric RCS Flow Measurement 19 Uncertainties 6 Cold Leg Elbow Tap Flow Uncertainty 22 7 Power Calorimetric Instrumentation 25 Uncertainties 8 Secondary Side Power Calorimetric 26 Measurement Uncertainties 4

iii m

LIST OF ILLUSTRATIONS

. FIGURE NUM8ER TITLE PAGE 1

RCS Flow Calorimetric Schematic 30 2 Power Calorimetric Schematic 31 P

l iv

WESTINGHOUSE REVISED THERMAL DESIGN PROCEDURE INSTRUMENT UNCERTAINTY METHODOLOGY FOR ALABAMA POWER FARLEY NUCLEAR PLANT UNITS 1 AND 2 (FOR RTD BYPASS LOOP ELIMINATION)

I. INTRODUCTION Four operating parameter uncertainties are used in the uncertainty analysis of the Revised Thermal Design Procedure (RTDP). These parameters are Pressurizer Pressure, Primary Coolant Average Temperature (Tavg)'

Reacto' Power, and Reactor Coolant System Flow. They are frequently monitored and several are used for control purposes. Reactor power is monitored by the performance of a secondary side heat balance (power calorimetric) once every 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br />. RCS flow is monitored by the performance of a precision flow calorimetric at the beginning of each cycle. Pressurizer pressure is a controlled parameter and the uncertainty reflects the control system. T avg is a controlled parameter via the temperature input to the rod control system and the uncertainty reflects this control system. This report is based on the elimination of RTD Bypass Loops in the design to measure hot and cold leg reactor coolant system temperatures and is applicable for 2660 and 2785 Mwt operation.

The RTOP(I4) is used to predict the plant's DNBR design 'i :it. The RTDP ,

methodology considers the uncertainties in the system operating plant parameters, fuel fabrication and nuclear and thermal parameters and includes the use of various DNB correlations. Use of the RTDP methodology requires that variances in the plant operating parameters be justified.

The purpose of the follawing evaluation is to define the specific Farley j Nuclear Plant instrument uncertainties for the four primary system operating parameters.

! Westinghouse has been involved with the development of several techniques

. to treat instrumentatton uncertainties. An early version (for D. C. Cook 2 and Trojan) used the methodology outlined in WCAP-8567 " Improved Thermal Design Procedure",0 ,2,3) which is based on the conservative assumption that the uncertainties can be described with uniform probability distributions.

Another approach (for McGuire and Catawba) is based on the more realistic assumption that the uncertainties can be described with random, normal, two sided probability distributions.(4) This approach is used to substantiate the

_ acceptability of the protection system setpoints for many Westinghouse plants, e.g., D. C. Cook 2(5), V. C. Summer, Wolf Creek, Millstone Unit 3 and others.

The second approach is now utilized for the determination of all instrumentation errors for both RTDP parameters and protection functions.

The uncertainty calculations in this report are based on a detailed review of Farley Nuclear Plant procedures for instrument calibration, heat balance calculations, and RCS flow measurement. The evaluation of heat balance uncertainties includes both the precision heat balance for RCS flow determination as well as the plant process computer heat balance used for the daily nuclear instrumentation alignment surveillance.

II. METHODOLOGY The methodology used to combine the error components for a channel is the square root of the sum of the squares of those groups of components which are statistically independent. Those errors that are dependent are combined arithmetically into independent groups, which are ther, systematically combined. Tne uncertainties used are considered to be random, two sided distributions. The sum of both sides is equal to the range for that paramster, e.g., rack drift is typically

[ ]+a,c, the range for this parameter is [ ]+a,c, This technique has been utilized before as noted above, and has been endorsed by the NRC staff (6,7,8,9) and various industry standards (10,ll),

)

The relationships between the error components and the ch6nnel instrument

, error allowance are variations of the basic Westinghouse Setpoint Methodologyjl2) and are defined as follows:

1. For precision parametor indication using.special test equipment or a DVM at.the input to the racke, CSA - ((SCA + SMTE + SD)2 + (SPE)2 + (STE)2+ (RDOUT)2)l/2 ,

+ BIAS. Eq. 1

'2. For parameter indication utilizing the plant process computer,-

CSA - ((SCA + SMTE + SD)2 + (SPE)2 + (STE)2 + (RCA + RMTE + RD)2

+ (RTE)2 + (10)2 + (A/0)2)l/2 + BIAS. Eq. 2

3. For parameters which have control sy. Stems, CSA - ((PMA)2 + (PEA)2 +(SCA + SMTE + SD)2 + (SPE)2 + (STE)2

+ (RCA + RMTE + RD + CA)2 + (RTE)2)l/2-+ BIAS. Eq. 3 where, CSA - Channel Allowance PMA - Process Measurement Accuracy PEA - Primary Element Accuracy SCA - Sensor Calibration Accuracy SMTE -

Sensor Measurement and Test Equipment Accuracy SPE -

Sensor Pressure Effects STE - Sensor Temperature Effects SD - Sensor Drift-RCA - Rack Calibration Accuracy RMTE -

Rack Heasurement and Test Equipment Accuracy RTE - Rack Temperature Effects RD - Rack Drift RDOUT -

Readout Device Accuracy (DVM or gauge)

ID - Computer Isolator Drift l~ A/D. - Analog to Digital Conversion Accuracy CA - Controller Accuracy.

i

The parameters above-are as defined in references 5 and 12 and are based on

.. SAMA Standard PMC 20.1,1973(I3). However, for ease in understanding they are paraphrased below:

PMA -

non-instrument related measurement errors, e.g., temperature stratification of a fluid in a pipe, '

PEA -

- errors due to a metering device, e.g., elbow, venturi, orifice, SCA - reference (calibration) accuracy for a sensor / transmitter, SPE -

change in input-output relationship due to a change in static pressure for a d/p cell, STE - change in input-output relationship due to a change in ambient temperature for a sensor / transmitter, SD -

change in input-output relationship over a period of tiine at reference conditions for a sensor / transmitter, RCA -

. reference (calibration) accuracy for all rack modules in loop or --

channel assuming the loop or channel is string calibrated, or tuned, to this accuracy.

RTE -

change in input-output relationship due to a change in ambient temperature for the rack modules, RD -

change in input-output relationship over a period of time at reference conditions for the rack modules, RDOUT -

the measurement accuracy of a special test local gauge, digital voltmeter or multimeter on its most accurate applicable range for the parameter measured,

ID -

-change in input-output relationship over a _ period of time at reference conditions for a control / protection signal -isolating device, A/D - allowance for conversion accuracy of an analog signal to a digital signal for process computer use, CA -

allowance for the accuracy of a controller, not including deadband.

BIAS -- a non-random uncertainty for a sensor / transmitter or a process parameter.

A more detailed explanation of the Westinghouse methodology noting the interaction of several parameters is provided in references 5 and 12.

4 III. INSTRUMENTATION UNCERTAINTIES

, The instrumentation uncertainties will be discussed first for the two parameters which are controlled by automatic systems -- Pressurizer Pressure, and RCS average temperature (Tavg). Then the development of the uncertainties for the RCS flow and the secondary side power calorimetric measurements will be discussed.

1. PRESSURIZER PRESSURE Pressurizer pressure is normally controlled automatically to simplify plant operation and to maintain pressure within the normal steady state envelope of operation assumed in the safety analysis. To ensure that pressure is restored within its limit following load changes and other expected transient operation, a 12 hour1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br /> surveillance of pressurizer pressure through instrument readout is included in the Technical Specifications.

Pressurizer pressure is controlled by comparison of the measured vapor space pressure and a reference value. Allowances are made for the transmitter and the process racks / controller. As noted on Table 1, the electronics uncertainty for this function is [ ]+a,c which corresponds to an accuracy of [ ]+a,c. In addition to the controller accuracy, an allowance is made for pressure overshoot or undershoot due to the interaction and thermal inertia of the heaters and spray. B:,nj on an evaluation of plant operation, an allowance of [ ]+a,c was made for this effect. Therefore, a total control system uncertainty of [

]+a,c is calculated, which results in a standard deviation of [

]+a,c (assuming a normal, two sided probability distribution).

I TABLE 1 PRESSURIZER PRESSURE CONTROL SYSTEM ACCURACY

+a,c SCA -

SMTE-STE -

SD -

BIAS =

RCA a RMTE-RTE -

RD -

CA -

+a,c ELECTRONICS UNCERTAINTY -

PLUS ELECTRONICS UNCERTAINTY -

PLUS CONTROLLER UNCERTAINTY -

_. J (e

This calculation is performed assuming that: _

+a,c EIMIAI e

t

2. T AVG Tavg is normally controlled nutomatically through the rod control system to simplify plart operation and to maintain Tavg within the normal steady; state envelope of operation assumed in the safety analysis. to ensure that temperature is restored within its limit following load changes and other expected transient operation, a 12 hour1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br /> periodic surveillance of RCS T avg through instrument readout is included in the Technical Specifications.

T pyg is controlled by a system that compares the median Tavg (from the_ Median Signal Selector) from the loops with a reference that is derived from the first stage turbine impulse chamber pressure. T avg IS the average of the narrow range TH and TC values. The median loop T avg is then used in the controller. Allowances are made (as noted on Table 2) for the RTDs, transmitter and the process racks / controller. The CSA for-this function is dependent on the type of RTD, pressure

- transmitter, and the location of the RTDs, i.e., in the RTD bypass manifold or in the hot and cold legs. Based on the assumption that 2 TH (with I failed hot leg RTD) and 1 TC cross-calibrated RTDs are used to calculate T avg and the RTDs are located in the hot and cold iegs, the-CSA for the electronics is [ ]+a,c. Assuming a

- normal, two sided probability distribution results in an electronics-standard deviation (si) of (- ]+a,c, L

However, this does not include the controller deadband of i 1.5 0 F.

The controller _ accuracy is the combination of the instrumentation accuracy and the deadband. The probability distribution for the deadband has been determined to be [

).+a,c The variance for the deadband

. uncertainty is_then:

(s2) "I l+ '

  • l Combining the variance for instrumentation and deadband results in a controller variance of: '

(sT) * (81) + (s2) "I 3+ '

With a controller sT = [ ]+ ' , the total uncertainty is

[ ]+a,c, TABLE 2 R0D CONTROL SYSTEM ACCURACY Tavg TURB PRES

+a,c PHA -

SCA -

SMTE-STE -

SD -

BIAS-RCA -

RMTE-RMTE-RTE -

RD =

CA -

l BIAS-

  1. RTDs USED - TH - 2 TC - 1

+a,c ELECTRONICS CSA -

ELECTRONICS SIGMA -

CONTROLLER SIGMA =

CONTROLLER BIAS -

CONTROLLER CSA =

l _ _

  • Includes the controller deadband of 1.5 0F.

This calculation was performed assuming that: +a,c l

4 i

i

3. BOS= FLOW RTDP and the plant Technical Specifications require three RCS flow

. surveillances: a total RCS flow measurement every fuel cycle (every 18 months) that is used to calibrate the RCS flow instrument channels; a monthly total RCS flow measurement; and a qualitative RCS ficw verification every 12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br /> to maintain RCS flow within the assumed safety analysis value. The 18 month RCS flow surveillance is satisfied by a precision RCS flow measurement; the monthly RCS flow surveillance is satisfied by a process computer measurement from the RCS flow instrument channels whose calibration is based on the 18 month precision RCS flow measurement; and the 12 hour1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br /> RCS flow surveillance is satisfied by control board RCS flow indicator readings. No drift is assumed in this error analysis for hot and cold leg RTDs and the feedwater flow transmitters used in the RCS flow measurement procedure. Six (6) month drift effects are included for feedwater temperature, steam pressure and pressurizer pressure measurements. It is also assumed that the calorimetric flow measurement is performed at the beginning of a cycle, i.e., no allowances have been made for mid cycle feedwater venturi fouling, and above 90% RTP.

The RCS flow measurement is performed by determining the steam generator thermal output (corrected for the RCP heat input and the loop's share of primary system heat losses) and the enthalpy rise (Delta-h) of the primary coolant. Assuming that the primary and secondary sides are in equilibrium, the RCS total vessel flow is the sum of the individual primary loop flows, i.e.,

WRCS - N(W L ).

Eq. 4 The individual primary loop volumetric flows are determined by

~

correcting the thermal output of the steam generator for steam generator blowdown (if not secured), subtracting the RCP heat addition, adding the loop's share of the primary side system losses, dividing by the primary side enthalpy rise and multiplying by the cold leg specific volume. The equation for this calculation is-l

.g.

i Wt - 3)10 5C - Op_f_(.Qt /N)M VC 1 (hg-h)C Eq. 5 where, WL = Loop flow (gpm)

A - 0.1247gpm/(ft/hr) 3 Qg3

- Steam generator thermal output (Btu /hr)

Qp -

RCP heat addition (Btu /hr)

QL

- Primary system net heat losses (Btu /hr)

V C

Specific volume of the cold leg at TC (ft3 /lb)

N - Number of primary side loops h

H

- Hot leg enthalpy (Btu /lb) h C

- Cold leg enthalpy (Btu /lb).

The thermal output of the steam generator is determined by a precision secondary side calorimetric measurement, which is defined as:

Q3 g - (h3 - h f)Wf Eq. 6 where, h

s

- Steam enthalpy (Btu /lb) h f

- Feedwater enthalpy (Btu /lb)

Wf -

Feedwater flow (lb/hr).

The steam enthalpy is based on measurement of steam generator outlet steam pressure, assuming saturated conditions. The feedwater enthalpy is based on the measurement of feedwater temperature and steam pressure.

The feedwater flow is determined t,y multiple measurements and the following calculation:

W f - (K)(Fa}((Pf )(d/p)}l/2 Eq. 7 where, W

7

- Feedwater loop flow K - Feedwater venturi flow coefficient F

a

- Feedwater venturi correction for thermal expansion pf - Feedwater density (lb/ft3) d/p - Feedwater venturi pressure drop (inches H 2O).

The feedwater venturi flow coefficient is the product of a number of constants including as-built dimensions of the venturi and calibration tests performed by the vendor. The thermal expansion correction is based on the coefficient of expansion of the venturi material and the difference between feedwater temperature and calibration temperature.

Feedwater density is based on the measurement of feedwater temperature and steam pressure. The venturi pressure drop is obtained from the output of the differential pressure cell connected to the venturi.

RCP heat addition is determined by calculation, based on the best estimate of coolant flow, pump head, and pump hydraulic efficiency.

The primary system net heat losses arc determined by calculation, considering the following system heat inputs and heat losses:

Charging flow Letdown flow Seal injection flow RCP thermal barrier cooler heat removal Pressurizer spray flow Pressurizer surge line flow Component insulation heat losses Component support heat losses CRDM heat losses.

A single calculated sum for 100% RTP operation is used for these losses or heat inputs.

The hot leg and cold leg enthalpies are based on the measurement of the hot leg temperature, cold leg temperature and pressurizer pressure. The cold leg specific volume is based on measurement of the cold leg tamperature and pressurizer pressure.

l l

The RCS flow measurement is thus based on the following plant measurements:

Steamline pressure (P3 )

Feedwater temperature (Tf )

Feedwater venturi d'fferential pressure (d/p)

Hot leg temperature (TH)

Cold leg temperature (TC )

Pressurizer pressure (Pp)

Steam generator blowdown (if not secured) and on the following calculated values:

Feedwater venturi flow coefficients (K)

Feedwater venturi thermal expansion correction (Fa)

Feedwater density (pf)

Feedwater pressure (Pf )

Feedwater enthalpy (hy)

Steam enthalpy (hs )

Moisture carryover (impacts hs )

Primary system net heat losses (QL)

RCP heat addition (Qp)

Hot-leg enthalpy (hg)

Cold leg enthalpy (hC )-

These measurements and calculations are presented schematically on Figure 1.

The derivation of the measurement errors and flow uncertainties on Table 5 are noted below.

Secondary Side The secondary side uncertainties are in four principal areas -- feedwater flow, feedwater enthalpy, steam enthalpy and RCP heat addition. These four areas are specifically identified on Table 5.

- for the measurement of feedwater flow, each feedwater venturl is calibrated by the vendor in a hydrauliss laboratory under controlled conditions to an accuracy of ( J+a,c. The calibration data which substantiates this accuracy is previded to the plant by the venoor. An additional uncertainty factor of [ ]+a,c 43 included for installation ef fects, resulting in a conservative overall flow coefficient (K) uncertainty of [ ]+a,c. Since the ralculated RCS 1000 flow is related to the calculated steam generator

'j thermal output which in turn is proportional to feedwater flow, the flow

  • ]4a,c. It should coefficient uncertainty is expressed cs [

be noted tP t no allowance is made for venturi fouling. The venturis should t.e inspected, and cleaned if necessary, prior to performance of the pre:ision measurement, if fouling is present but not removed, its

! effects must be treated as a flow hias.

The ure.ertainty applied to the feedwater venturi thermal expansion

~'

correction (f )a is based on the uncertainties of the measured feedwater temperature and the coefficient of thermal expansion for the venturi mr,terial, usually 304 stainless steel, for this material, a change of i 13.0 f Oin the nominal feedwater temperature range changes af by 1 0.026 % and the steam generator thermal output by the same amount.

Based on data introduced into the A5HE Code, the uncertainty inaf for 304 stainless steel is i S %. This results in an additienal uncertainty of ( )+a,c in feedwater flow.

m Using the 1967 ASME Steam Tables it is possible to determine the sensitivities of various parameters to changes in feedwater temperature and pressure. Table 3 notes the instrument uncertainties for the hardware used to perform the measurements. Table 4 lists the various sensitivities. As can be seen on Table 4, feedwater temperature uncertainties have an impact on venturi f a, feedwater density and feedwater enthalpy. Feedwater pressure uncertainties impact feedwater density and feedwater enthalpy.

3 13

Feedwater venturi d/p uncertainties are converted to % feedwater flow using the following conversion factor;

% flow - (d/p uncertainty)(1/2)(transmitter span /100)2 The feedwater flow transmitter span is [ )+a,c of nominal flow.

Using the 1967 ASME Steam Tables again, it is possible to determine the sensitivity of steam enthalpy to changes in steam pressure and steam quality. Table 3 notes the uncertainty in steam pressure and Table 4 provides the sensitivity. For steam quality, the Steam Tables were used to determine the sensitivity at a moisture content of ( )+a,c. This value is noted on Table 4.

The net pump heat uncertainty is derived from the combination of the primary system net heat losses and pump heat addition and are summarized for a three loop plant as follows:

System heat lost.es -2.0 MWt Component conduction and convectior losses -1.4 Pump heat adder ilhQ Net Heat input to RCS + 6.6 MWt The uncertainty on system heat losses, which is essentially all due to charging and letdown flows, has been estimated to be [ ]+a c of the calculated value. Since direct measurements are not possible, the uncertainty on component conduction and convection losses has been assumed to be [ ]+a.c of the calculated value. Reactor coolant pump hydraulics are known to a relatively high confidence level, supported by system hydraulics tests performed at Prairie Island II and by input power measurements from several plants, therefore, the uncertainty for t5e pump heat addition is estimated to be [ ]+a,c of the best estimate value.

Considering these parameters as one quantity, which is designated the net pump heat uncertainty, the combined uncertainties are less than

[ ]+a,c of the total, which is [ ]+a,c of cc e power, i

Primary Side The primary side uncertainties are in three principal areas hot leg enthalpy, cold leg enthalpy and cold leg specific volume. These are specifically noted on Table 5. Three primary side parameters are actually measured, Ty and T;, and pressurizer pressure. Hot leg enthalpy is influenced by Tg, pressurizer pressure and hot leg temperature streaming.

The uncertainties for the instrumentation are noted on Table 3, the sensitivities are provided on Table 4. The hot leg streaming is split into random and bias (systematic) components, for the Farley units with RTDs located in thermowells placed in the scoops (bypass manifolds eliminated), the streaming uncertainty is [ 1+a,c random and [ ]+a,c systematic components.

The cold leg enthalpy and specific volume uncertainties are impacted by TC and pressurizer pressure. Table 3 notes the TC instrument uncertainty and Table 4 provides the sensitivities.

Noted on Table 5 is the plant specific RlD cross-calibration systematic allowance. When necessary, an allowance is made for a systematic temperature error due to the RTD cross-calibration procedure. No allowance was necessary for this plant.

Parameter dependent effects are identified on Table 5. Westinghouse has determined the dependent sets in the calculation and the direction cf interaction, i.e., whether components in a dependent set are additive or subtractive with respect to a conservative calculation of RCS flow. The same work was performed for the inctrument bias values. As a result, the calculation explicitly accounts for dependent effects and biases with credit taken for sign (or direction of impact).

I Using lable 5, the 3 loop uncertainty equation (with biases) is as follows:

-+a,c Based on the number of loops, number, type, measurement method of RTDs, the averaging of the three hot leg temperatures, and the vessel Delta-T, the flow uncertainty for the precision flow calorimetric is:

  1. of loops flow uncertainty (% flow)

-4ac 3

S

TABLE 3 FLOW CALORIMETRIC INSTRUMENTATION UNCERTAINTIES

(% SPAN) FW TEMP FW PRESS FW d/p STM PRESS in T C

PRZ PRESS 4a,c SCA -

SMTE-SPE a STE -

SD -

R/E -

RDOUT-BIAS.

CSA -

  1. OF INST USED 3 1 2 or (l) psig(2) % d/p(3) psig(l) Of(4) O f(4) psig(5)

INS 1 SPAN - 500. 2000. 120% 1200. 120. 120. 800.

INST UNC. - -

+a,c (RANDOM)-

INST UNC.

(BIAS)

NOMINAL - 4370F 893 psia 100% flow 793 psia 610.90 F 543.5 0F 2250 psia Notes:(1) Based on permanently installed plant instrumentation and read from the plant computer.

(2) A steam pressure measurement is read from the plant computer and is substituted for a feedwater pressure measurement. A conservative uncertainty value is usod.

(3) Measured with a Barton transmitter. This does not include the venturi uncertainty.

(4) Temperature measured with DVH at the input to Westinghouse process instrumentation using an RTD test rig.

(5) Based on permanently installed plant instrumentation and read from the plant computer. The calculation is based on control board

. indicators.

These calculations were performed assuming that: +a.c e

N M

TABLE 4 FLOW CALORIMETRIC SENSITIVITIES FEEDWATER FLOW TEMPERATURE KATERIAL -

DENSITY TEMPERATURE -

PRESSURE -

DELTA P =

FEEDWATER ENTHALPY TEMPERATURE -

PRESSURE -

h = 1199.6 BTU /LBM 3

416.4 BTU /LBM hr(SG)

Dh - 7B3.2 BTU /LBM STEAM ENTHALPY PRESSURE -

MOISTURE -

HOT LEG ENTHALPY TEMPERATURE -

PRESSURE -

hg 629.1 BTV/LBM bc 539.1 BTV/LBM Dh(VESS) 90.0 BTU /LBM Cp(TH ) =

1.492 BTV/LBM Of COLD LEG ENTHAI.PY TEMPERATURE -

PRESSURE -

Cp(TC ) =

1.228 BTV/LBM OF COLD LEG SPECIFIC VOLUME

+a c TEMPERATURE -

PRESSURE -

4

i

. TABLE 5 CALORIMETRIC RCS FLOW MEASUREMENT UNCERTAINTIES

- (Page 1 of 2)

COMPONENT INSTRUMENT ERROR FLOW UNCERTAINTY FEEDWATER FLOW +a c VENTURI THERMAL EXPANSION COEFFICIENT TEMPERATURE MATERIAL DENSITY TEMPERATURE PRESSURE DELTA P FEEDWATER ENTHALPY TEMPERATURE PRESSURE STEAM ENTHALPY PRESSURE MOISTURE NET PUMP HEAT ADDITION HOT LEG ENTHALPY TEMPERATURE STREAMING, RANDON STREAMING, SYSTEMATIC PRESSURE COLD LEG ENTHALPY TEMPERATURE PRESSURE COLD LEG SPECIFIC VOLUME TEMPERATURE PRESSURE RTD CROSS-CAL SYSTEMATIC ALLOWANCE

  • ** , +, ++ INDICATE SETS OF DEPENDENT PARAMETERS 4

i I

TABLE 5 (CONTINUED)

. CALORIMETRIC RCS FLOW MEASUREMENT UNCERTAINTIES (Page 2 of 2)

COMPONENT FLOW UNCERTAINTY BIAS VALUES - --

+a,c FEEDWATER PRESSURE DENSITY ENTHALPY STEAM PRESSURE ENTHALPY PRESSURIZER PRESSURE ENTHALPY - HOT LEG ENTHALPY - COLD LEG SPLCIFIC VOLUME - COLD LEG FLOW BIAS TOTAL VALUE

+A,C SINGLE LOOP UNCERTAINTY (WITHOUT BIAS VALUES)

N LOOP UNCERTAINTY (WITHOUT BIAS VALUES)

N LOOP UNCERTAINTY (WITH BIAS VALUES) 9 9

l

4 i

The precision flow calorimetric may be used as a reference for the normalization of the cold leg elbow taps. Table 6 notes the instrument uncertainties for normalization of the elbow taps, assuming one elbow tap per

~

loop. The d/p transmitter uncertainties are converted to % flow on the same basis as the feedwater venturi d/p. The elbow tap uncertainty is thtn combined with the precision flow calorimetric uncertainty. This combination of uncertainties results in the following total flow uncertainty :

  1. of loops flow uncertainty '% flow) 3 1 2.2 The corresponding value used in RTDP is:
  1. of loops standard deviation (% flow)

+a,c 3

e

TABLE 6

! C0?D LEG ELBOW TAP FLOW UNCERTAINTY INSTRUMENT UNCERTAINTIES

% d/p SPAN  % FLOW

+a,c DMA -

Pil -

SCA -

SPE -

STE -

SD -

RCA -

RMTE-RTE -

RD -

10 -

A/D -

RDOUT-BIAS =

FLOW CALORIN. BIAS -

FLOW CALORIMETRIC -

INSTRUMENT SPAN -

SINGLE LOOP ELBOW TAP FLOW UNC -

N LOOP ELBOW TAP FLOW UNC -

N LOOP RCS FLOW UNCERTAINTY (WITHOUT BIAS VALUES)

N LOOP RCS FLOW UNCERTAINTY - --

(WITH BIAS VALUES) - 2.2 e

l

4. REACTOR POWER Generally a plant performs a primary / secondary side heat balance once

. every 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> when power is above 15% Rated Thermal Power. This heat balance is used to verify that the plant is operating within the limits of the Operating License and to adjust the Power Range Neutron Flux channels when the difference between the NIS and the heat balance is greater than that required by the plant Technical Specifications.

l l

Assuming _that the primary and secondary sides are in equilibrium; the core power is determined by summing the thermal output of the steam generators, correcting the total secondary power for steam generator blowdown (if not secured), subtracting the RCP heat addition, adding the primary side system losses, and dividing by the core rated Btu /hr at full power. The equation for this calculation is:

RP = (fN)(O SC - Op 3_(OL /N)))(100)

H Eq. 8 where, RP = Core power (% RTP)

N = Number of primary side loops [

Qg3

= Steam generator thermal output (BTU /hr) as defined in Eq. 6 Qp = RCP heat adder (Btu /hr) as defined in Eq. 5 QL

= Primary system net heat losses (Btu /br) as defined in Eq. 5 H = Core rated Btu /hr at full power.-

For the purposes of this uncertainty analysis (and based on H noted above) it is assumed that the plant is at 100% RTP when the measurement is taken. Measurements performed at lower power levels will result in different uncertainty values. However, operation at lower power levels results in increased margin to DNS far in excess of any margin losses due to increased measurement uncertainty.

The secondary side power calorimetric equations and effects are the same as those noted for the precision flow calorimetric (secondary side 4

m 1

portion), cquations 6 and 7. Table 7 provides the instrument uncertainties for those measurements performed. Since it is necessary to make this determination daily, it has been assumed that the plant

. process computer will be used for the measurements. The sensitivities calculated are the same as those noted for the secondary side on Table

4. As noted on Table 8, Westinghouse has determined the dependent sets in the calculation and the direction of interaction. This is the same as that performed for the RCS flow calorimetric, but applicable only to power. The same was performed for the bias values noted. It should be noted that Westinghouse does not include any allowance for feedwater venturi fouling. The effect of fouling is to result in an indicated power higher than actual, which is conservative.

Using the power uncertainty values noted on Table 8, the 3 loop uncertainty (with bias values) equation is as follows:

+a,c Based on the number of loops and the instrument uncertainties for the four parameters of feedwater temperature, feedwater pressure, feedwater flow and steam pressure, the power measurement uncertainty for the secondary side power calorimetric is:

  1. of loops power uncertainty (% RTP)

+ac 3

9 e

TABLE 7 DOMER CALORIMETRIC INSTRUMENTATION UNCERTAINTIES

(% SPAN) FW TEMP FW PRESS FW d/p STM PRESS

+a,c SCA =

SMTE-SPE -

STE -

SD -

BIAS-RCA -

RMTE-RTE -

RD =

ID -

A/D -

CSA =

0F (l) psig(2) % d/p(3) psjg(1)

INST SPAN - 500. 2000. 120% Flow 1200.

INST UNC -- --

d a ,c (RAND 0H) -

INST UNC (BIAS)

NOMINAL - 4410F 644 psia 100% 744 psia Notes:

(1) Based on permanently installed plant instrumentation and read from the plant computer.

(2) A steam pressure measurement is substituted for a feedwater pressure measurement. A conservative uncertainty value is used.

(3) Based on permanently installed plant instrumentation (protection channel feedwater flow) and read from the plant computer.

Normally the daily power calorimetric measurement is performed by reading the local Barton d/p transmitter. The feedwater flow channel represents a conservative uncertainty calculation.

TABLE 8 SECONDARY SIDE POWER CALORIMETRIC HEAS!!REMENT UNCERTAINTIES COMPONENT INSTRUMENT ERROR PCWER UNCERTAINTY

+8,C FEEDWATER FLOW VENTURI THERMAL EXPANSION COEFFICIENT TEMPERATURE KATERIAL DENSITY TEMPERATURE PRESSURE DELTA P FEEDWATER ENTHALPY TEMPERATURE PRESSURE STEAM ENTHALPY PRESSURE MOISTURE NET PUMP HEAT ADDITION BIAS VALUES FEEDWATER DELTA P FEEDWATER PRESSURE DENSITY EN1HALPY STEAM PRESSURE ENTHALPY POWER BIAS TOTAL VALUE

, INDICATE SETS OF DEPENDENT PARAMETERS SINGLE LOOP UNCERTAINTY (WITHOUT BIAS VALUES)

N LOOP UNCERTAINTY (WITHOUT BIAS VALUES)

N LOOP UNCERTAINTY (WITH BIAS VALUES)

G

IV. CONCLUSIONS The preceding sections provide the methodology for what Westinghouse believes is a reasonable means of accounting for instrument uncertainties for pressure, temperature, power and flow. The plant-specific instrumentation has been reviewed for farley Nuclear Plant Units 1 and 2 and the uncertainty calculations are completed based on RTD Bypass Loop Elimination. These uncertainty values or more conservative values are used in the RTDP analysis.

9

REFERENCES

1. Westinghouse letter NS-CE-1583, C. Eiche1dinger to J. f. Stolz, NRC, dated 10/25/77.
2. Westinghouse letter NS-PLC-Sill, T. H. Andetson to E. Case, NRC, dated 5/30/78.
3. Westinghouse letter NS-TMA-1837, T. M. Anderson to S. Varga, NRC, dated 6/23/78.
4. Westinghouse letter NS-EPR-2577. E. P. Rahe Jr. to C. H. Berlinger, NRC, dated 3/31/82.
5. Westinghouse Letter NS-TMA-1835, T. M. Anderson to E. Case, NRC, dated 6/22/78.
6. NRC letter, S. A. Varga to J. Dolan, Indiana and Michigan Electric Company, dated 2/12/81.
7. NUREG-0717 Supplement No. 4, Safety Evaluation Report related to the operation of Virgil C. Summer Nuclear Station Unit No. 1, Docket 50-395, August, 1982.
8. Regulatory Guide 1.105 Rev. 2, " Instrument Setpoints for Safety-Related Systems", dated 2/86.
9. NUREG/CR-3659 (PNL-4973), "A Mathematical Model for Assessing the Uncertainties of Instrumentation Measurements for Power and flow of PWR Reactors",2/85.
10. AF'il/ANS Standard 58.4-1979, " Criteria for Technical Specifications for Nuclear Power Stations"
11. ISA Standard S67.04,1982, "Setpoints for Nuclear Safety-Related Instrumentation Used in Nuclear Power Plants"
12. Tuley, C. R., Miller, R. B., " Westinghouse Setpoint Methodology for Control and Protection Systems'. IEEE Transactions on Nuclear Science, February, 1986, Vol . NS-33 No.1, pp. 684-687.
13. Scientific Apparatus Manufacturers Association, Standard PMC 20.1, 1973,

" Process Measurement and Control Terminology".

14. Westinghouse WCAP ll397-P-A, " Revised Thermal Design Procedure", dated April, 1989.

4

i FIGURE 1 RCS FLOW CALORIMETRIC SCHD% TIC TC l l Pp ln.

TH I l Ps Pf j nTf I Ap

/

hc hH hs hf of Fa K

/

ah W f

IP

> QSG  :

g - . T, .-  % Measured O Calculated 0 1 r

__ Mass WL

'I

= vc - 101

~

I P

  • Three hot leg temperatures per loop are measured and averaged

{  : D eer Loops

    • 0ne temperature per loop is measured y RCS Yolumetric Flow I

FIGURE 2 POWER CALOR! METRIC SCHEMATIC I l P l T j j op j s f f A q l

h h p 3 f pf a E

V W 2 f

y 0 - measured O

sa 0 - calculated 4

-e _

Other Loops 4+

O Op L

Core Power

~

.- . _ _ _ _ _ _ _ _ _ _ _ - - _ _ _ -